BUGSAT 1, 40014
Orbit data source: Space-Track
BUGSAT 1, 40014 is a payload satellite owned by Satellogic SA (AR) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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40014 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ARGNRelated business
Manufacturer
Satellogic SA
Mission
Operational Commercial Imaging
Bus & Motor
BUGSAT, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.263 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 BUGSAT 1
1 40014U 14033E 25289.57247253 .00006921 00000-0 40008-3 0 9994
2 40014 98.0622 3.2728 0028914 291.9044 67.9111 15.12289015618973Epoch: 2025-10-16T13:44Z
TLE epoch observation values (Epoch: 2025-10-16T13:44:21.626Z)
Latitude
-0.00008°
Longitude
131.85244°
Altitude
524.819 km
Speed
7.605 km/s
True Right ascension
00h 13m 05s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:36:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.19 km
Perigee altitude
506.263 km
Semi-major axis
6,904.363 km
Eccentricity
0.00289
Inclination
98.0622°
RAAN
3.2728°
Arg. of periapsis
291.9044°
True anomaly
68.21853°
Mean anomaly
67.9111°
Eccentric anomaly
68.06477°
Mean motion
3.78319 °/min
Orbital period
95.16 mins
BSTAR
0.00040008
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Other satellites on launch #33 in the year 2014 (2014-06-19 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.BUGSAT 1 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-17 04:10:57.031Z | 111.617° ESE | 2025-10-17 04:12:57.031Z | 76.691° E | 19.328° | 2025-10-17 04:15:57.031Z | 21.942° NNE |
| 4 mins | 2025-10-17 05:45:57.031Z | 227.851° WSW | 2025-10-17 05:46:57.031Z | 250.302° W | 23.028° | 2025-10-17 05:49:57.031Z | 313.927° NW |
| 4 mins | 2025-10-17 17:19:57.031Z | 58.172° ENE | 2025-10-17 17:21:57.031Z | 110.76° ESE | 25.465° | 2025-10-17 17:23:57.031Z | 149.98° SSE |
| 4 mins | 2025-10-17 18:53:57.031Z | 323.068° NNW | 2025-10-17 18:55:57.031Z | 284.018° WNW | 18.045° | 2025-10-17 18:57:57.031Z | 250.796° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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